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本文通过在直流连续式跨音速FL-7风洞进行的一次气动加热试验,针对某型号飞机模型介绍了一种接触式与非接触式测量相结合的表面蒙皮温度场测量方法,并针对测量数据进行了初步分析。试验结果证明这种测量方案是可行的,有效的。
In this paper, an aerodynamic heating test is carried out in a DC continuous transonic FL-7 wind tunnel. A method for measuring the temperature field of the surface skin is presented based on a combination of contact and non-contact measurement for a certain aircraft model. Data for a preliminary analysis. The test results prove that this measurement scheme is feasible and effective.